Aerodynamics of missiles with slotted fin configurations-Reference-Cited by-同舟云学术

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Aerodynamics of missiles with slotted fin configurations

Published:1991-01-07 Issue: Volume: Page:
ISSN:
Container-title:29th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

ABATE GREGG¹,WINCHENBACH GERALD¹

Affiliation:

1. USAF, Armament Laboratory, Eglin AFB, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-676

Reference14 articles.

1. THE EFFECT OF FIN SLOTS AND FIN TABS ON THE DYNAMIC STABILITY CHARACTERISTICS OF THE NAVY LOW DRAG BOMB

2. Subsonic and transonic aerodynamics of a wraparound fin configuration

3. Roll motion of a wraparound fin configuration at subsonic and transonic Mach numbers

4. Aerodynamics of missiles with offset fin configurations

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Comparison of Flow field in the proximity of A Single Planar & Wrap-around Fin;International Journal of Aviation, Aeronautics, and Aerospace;2019

2. Spinning Tail Aerodynamics of a Low Cost Precision Guided Missile;21st AIAA Applied Aerodynamics Conference;2003-06-21

3. Experimental investigation of supersonic wrap-around fin aerodynamic Mach number effects;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

4. Effects of Mach Number on Supersonic Wraparound Fin Aerodynamics;Journal of Spacecraft and Rockets;1998-11

5. Magnus Effects on Stability of Wraparound-Finned Missiles;Journal of Spacecraft and Rockets;1998-07

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